BFGoodrich | The Boeing Company Airworthiness Directives

4 ADs indexed for BFGoodrich | The Boeing Company aircraft.

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85-06-02

final rule

Airworthiness Directives; BF GOODRICH: Applies to BF Goodrich Main Landing Gear Wheel Assemblies

Unsafe Condition: Failure of certain BF Goodrich wheel assemblies due to tie bolt nut cracks.

Effective: Mar 19, 1985 Category: appliance Compliance: Within 50 flight hours after the effective date of this AD for inspection and replacement of crac...

Why matched: Airworthiness Directives; BF GOODRICH: Applies to BF Goodrich Main Landing Gear Wheel Assemblies

Technical illustration of an aircraft landing gear and wheel assembly
Problem area Landing gear

84-24-04 EMERGENCY

emergency

Airworthiness Directives; BF GOODRICH: Applies to BF Goodrich Emergency Evacuation Slide/Rafts

Unsafe Condition: Failure of the girt bar attachment assemblies could result in the emergency evacuation slide/rafts not deploying properly.

Effective: Dec 17, 1984 Category: appliance Compliance: Within the next 15 days after the effective date of this airworthiness directive

Why matched: Airworthiness Directives; BF GOODRICH: Applies to BF Goodrich Emergency Evacuation Slide/Rafts

83-22-08 EMERGENCY

emergency

Airworthiness Directives; B.F. GOODRICH: Applies to B.F. Goodrich Emergency Evacuation Slide/Rafts

Unsafe Condition: The B.F. Goodrich Emergency Evacuation Slide/Rafts P/Ns 7A1340 series, 7A1342 series, 7A1371 series, and 7A1373 series may experience undetected deterioration, leading to potential failure of the s...

Effective: Nov 15, 1983 Category: appliance Compliance: Within 20 calendar days after the effective date for specific serial numbers (G001-G289 and G001-...

Why matched: Airworthiness Directives; B.F. GOODRICH: Applies to B.F. Goodrich Emergency Evacuation Slide/Rafts

74-24-10

final rule

Airworthiness Directives; B.F. GOODRICH ENGINEERED SYSTEMS COMPANY: Applies Only To B. F. Goodrich Main Wheel Assembly P/N 3-1306 Manufactured Under Technical Standard Order (TSO-C26b)

Unsafe Condition: Possible failures in the hub area of the inboard wheel half, P/N 10-1202, at the second tire change due to forging defects.

Effective: Nov 27, 1974 Category: appliance Compliance: Within 500 hours' time in-service after November 27, 1974, or before further flight if the second...

Why matched: Airworthiness Directives; B.F. GOODRICH ENGINEERED SYSTEMS COMPANY: Applies Only To B. F. Goodrich Main Wheel Assembly P/N 3-1306 Manufactured Under Technical Standard Order (TSO-C26b)

Technical illustration of an aircraft landing gear and wheel assembly
Problem area Landing gear

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